| 1 |
NACA-TN-614
Fuselage-drag tests in the variable-density wind tunnel: streamline bodies of revolution, fineness ratio of 5 / Abbott, Ira H
Washington, DC (USA) : National Advisory Committee for Aeronautics , 1937.9
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| 2 |
NACA-TN-2138
Analytical and experimental investigation of adiabatic turbulent flow in smooth tubes / Deissler, Robert G.
Washington, DC (USA) : National Advisory Committee for Aeronautics , 1950.7.1
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| 3 |
NACA-TN-3133
The free-stream boundaries of turbulent flows / Corrsin, Stanley, Kistler, Alan L.
Washington, DC (USA) : National Advisory Committee for Aeronautics , 1954.1
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| 4 |
NACA-TN-2173
Density fields around a sphere at mach numbers 1.30 and 1.62 / Gooderum, Paul B., Wood, George P.
Washington, DC (USA) : National Advisory Committee for Aeronautics , 1950.8
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| 5 |
NACA-TN-2517
An Investigation of Aircraft Heaters - XXXVII - Experimental Determination of Thermal and Hydrodynamical Behavior of air flowing along a flat plate containing turbulence promoters / Boelter, L.M.K. [et al.]
Washington, DC (USA) : National Advisory Committee for Aeronautics , 1951.10
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| 6 |
NACA-TN-2629
Analytical and experimental investigation of fully developed turbulent flow of air in a smooth tube with heat transfer with variable fluid properties / R.G. Deissler, C.S. Eian
Washington, DC (USA) : National Advisory Committee for Aeronautics , 1952.2
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